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P200 Performance

 

Pioneer Aviation P200 Microlite

PIONEER AVIATION LAUNCH MICROLIGHT VERSION OF P200

A‘REAL’ AEROPLANE EXPERIENCE IN A MICROLIGHT!

P200 microlitePioneer Aviation’s new microlight version of the P200 made its debut appearance at the Popham International Microlight event. (August 2/3rd 2008)

Based on Italian Alpi Aviations popular P200 2 place, low wing, fixed tricycle undercarriage design, of which over 200 are already flying in Europe, the P200 Microlight has been developed to meet LAA microlight standard by Pioneer’s Managing Director Frank Cavaciuti.

The P200 Microlight is of quality wooden construction with fabric covering and is powered by the proven Rotax 912 engine. The aircraft is claimed to have excellent all round visibility, good aerodynamic characteristics and excellent performance and handling. It cruises at 115 mph on a fuel burn of 14.7 litres an hour offering a range of 350nm on a full tank (54 Litres).  Short field performance is an excellent 100 metres take off and landing run.

Pioneer’s Frank Cavaciuti said after the show, “ We were delighted with the response to P200 Microlight both from pilots and Microlight flying school operators and we are confident several firm orders will result from its initial appearance. Initially the aircraft will be available in advanced kit form for self-build (under the 51% rule) at around £37,000 including VAT but we are actively pursuing the necessary approvals to supply the aircraft ready to fly.”

The new Pioneer 200 Microlight represents a breakthrough in quality and value in the UK microlight market offering.

  • Excellent performance and handling
  • Comfortable well-equipped interior
  • Steerable nose wheel
  • Electric trim
  • 115 mph cruise
  • 14.7 litres per hour @75% power
PERFORMANCE  
Engine Rotax 912 80hp
Propellers

fixed PITCH  2 blade   

Max speed 116 kts/ 134 mph
Cruise speed (75% power) 100kts/115 mph
Stall speed 35kts/40mph
Take-off/Landing distance 100m
Best rate of climb speed 59 kts/68 mph
Best angle of climb speed 49kts/56mph
Rate of climb 985’/min
Roll rate 90 degrees/sec
Range @ 75% power 350 km
Fuel consumption @ 75% power 14.7lt/hr
Service ceiling 16,400ft
All figures based on MAUW of 450kgs
DIMENSIONS  
Fuselage length 6.15m
Wingspan 7.55m
Cabin width 1.05m
Fuel tank capacity 54 lt
Baggage allowance 20kgs
Baggage space 226l
Wing area 10.5 mē
Glide ratio 11/1
G limits +4/-2g
G limits including safety factor  +6g/ -3g
Empty weight 290 kgs
Gross weight 520 Kgs
 

 

More information about the P200 Microlight and arrangements for trial flights are available from Frank Cavaciuti at Pioneer Aviation on 07957 846849
Last modified: August 06, 2008